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FR936071A - Device for piloting an aircraft equipped with an even number of coaxial rotary airfoils - Google Patents

Device for piloting an aircraft equipped with an even number of coaxial rotary airfoils

Info

Publication number
FR936071A
FR936071A FR936071DA FR936071A FR 936071 A FR936071 A FR 936071A FR 936071D A FR936071D A FR 936071DA FR 936071 A FR936071 A FR 936071A
Authority
FR
France
Prior art keywords
piloting
even number
aircraft equipped
coaxial rotary
rotary airfoils
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
Other languages
French (fr)
Inventor
Louis Breguet
Rene Devillers
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed filed Critical
Application granted granted Critical
Publication of FR936071A publication Critical patent/FR936071A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR936071D 1946-11-09 1946-11-09 Device for piloting an aircraft equipped with an even number of coaxial rotary airfoils Expired FR936071A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR936071T 1946-11-09

Publications (1)

Publication Number Publication Date
FR936071A true FR936071A (en) 1948-07-08

Family

ID=9457148

Family Applications (1)

Application Number Title Priority Date Filing Date
FR936071D Expired FR936071A (en) 1946-11-09 1946-11-09 Device for piloting an aircraft equipped with an even number of coaxial rotary airfoils

Country Status (1)

Country Link
FR (1) FR936071A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1163156B (en) * 1960-10-01 1964-02-13 Boelkow Entwicklungen Kg Rotary wing aircraft
DE1270409B (en) * 1965-05-17 1968-06-12 Wagner Josef Device for direction control for helicopters with two coaxial load-bearing rotors running in opposite directions
US3521971A (en) * 1968-07-17 1970-07-28 United Aircraft Corp Method and apparatus for controlling aircraft
US3554467A (en) * 1968-02-19 1971-01-12 Universal Helicar Co Counterrotating rotor transmission for helicoptors
US4047838A (en) * 1976-03-22 1977-09-13 United Technologies Corporation Blade pitch control mechanism for helicopters
EP0038441A1 (en) * 1980-04-18 1981-10-28 Juan Campos Herruzo Rotor blade pitch control for helicopter with coaxial rotors

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1163156B (en) * 1960-10-01 1964-02-13 Boelkow Entwicklungen Kg Rotary wing aircraft
DE1270409B (en) * 1965-05-17 1968-06-12 Wagner Josef Device for direction control for helicopters with two coaxial load-bearing rotors running in opposite directions
US3554467A (en) * 1968-02-19 1971-01-12 Universal Helicar Co Counterrotating rotor transmission for helicoptors
US3521971A (en) * 1968-07-17 1970-07-28 United Aircraft Corp Method and apparatus for controlling aircraft
US4047838A (en) * 1976-03-22 1977-09-13 United Technologies Corporation Blade pitch control mechanism for helicopters
EP0038441A1 (en) * 1980-04-18 1981-10-28 Juan Campos Herruzo Rotor blade pitch control for helicopter with coaxial rotors
US4367063A (en) * 1980-04-18 1983-01-04 Herruzo Juan C Pitch control mechanism for coaxial helicopter steering

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